JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

このアイテムに関連するファイルはありません。

タイトルマイクロ波放電式中和器の電子引出に関する3次元Hybrid-PIC解析
その他のタイトルThree-dimensional Hybrid-PIC Analysis on Electron Extraction of a Microwave Neutralizer
著者(日)窪田, 健一; 渡邊, 裕樹; 山本, 直嗣; 中島, 秀紀; 宮坂, 武志; 船木, 一幸
著者(英)Kubota, Kenichi; Watanabe, Hiroki; Yamamoto, Naoji; Nakashima, Hideki; Miyasaka, Takeshi; Funaki, Ikkoh
著者所属(日)宇宙航空研究開発機構航空本部(JAXA); 首都大学東京; 九州大学; 九州大学; 岐阜大学; 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)
著者所属(英)Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA); Tokyo Metropolitan University; Kyushu University; Kyushu University; Gifu University; Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
発行日2015-10-05
発行機関など日本航空宇宙学会
Japan Society for Aeronautical and Space Sciences
刊行物名日本航空宇宙学会論文集
Journal of the Japan Society for Aeronautical and Space Sciences
63
5
開始ページ197(23)
終了ページ203(29)
刊行年月日2015-10-05
言語jpn
eng
抄録A microwave neutralizer composed of a cylindrical discharge chamber (18 mm in inner diameter) and an L-shaped antenna through which a microwave power of 8W is fed into a working gas was analyzed by a three-dimensional Hybrid-PIC solver to realize the simulation in ion's time/space scale. The microwave heating of electrons was analyzed with another electromagnetic PIC solver, and the obtained microwave power absorption rate was utilized in the Hybrid-PIC solver. Compared with the experimental result, the relative error of the simulated discharge current was about 2%, whereas the error depends on a coefficient in an anomalous resistivity model. The ion density has a peak about 3.34×10(exp 18) per cubic m near the antenna tip, which results in the high ion current (per unit area) into the antenna and the front yoke. Ion number density about 10(exp 18) per cubic m is also kept inside the orifice due to Townsend ionization processes, and it was found that the ions produced near the orifice exit are pushed back toward upstream region due to the potential gradient, and contribute to the electron extraction.
内容記述形態: 図版あり
Physical characteristics: Original contains illustrations
キーワードElectric Propulsion; Ion Engine; Neutralizer; Microwave; Numerical Simulation
資料種別Journal Article
NASA分類Spacecraft Propulsion and Power
ISSN1344-6460
NCIDAA11307372
SHI-NOAA1540301004
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/558575


このリポジトリに保管されているアイテムは、他に指定されている場合を除き、著作権により保護されています。